BendixKing KT 74 ADS-B OUT ENABLED MODE S TRANSPON

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KT 74 Pilot's Guide
D201308000036
Title Rev 0 Dec 2013
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© Honeywell International Inc. Do not copy without express permission of Honeywell
KT 74 ADS-B
OUT ENABLED
MODE S
TRANSPONDER
PILOT'S GUIDE
KT 74 Pilot's Guide
Record of Revisions
D201308000036 Page RR 1 Rev 0 Dec 2013
© Honeywell International Inc. Do not copy without express permission of Honeywell
Revision History and Instructions
Manual KT 74 ADS-B Out Enabled Mode S Transponder Pilot's
Guide
Revision 0
Summary This is a new release.
Record of Revisions
REVISION
NUMBER
REVISION DATE 0
DEC, 2013
KT 74 Pilot's Guide
D201308000036
Table of Contents Rev 0 Dec 2013 Page TC 1
© Honeywell International Inc. Do not copy without express permission of Honeywell
Table of Contents Section Page
1. Operation ................................................................................. 1-1
1.1 Introduction ...................................................................... 1-1 1.2 Front Panel Controls and Functions ................................ 1-2 1.3 Display ............................................................................. 1-2 Light Sensor .................................................................... 1-3 1.4 Mode Knob ...................................................................... 1-4 1.5 Push Buttons ................................................................... 1-5 Squawk Code Entry ......................................................... 1-6 1.6 Functions ......................................................................... 1-6 Flight Timer ...................................................................... 1-7 Stopwatch ........................................................................ 1-8 Flight ID Entry .................................................................. 1-8 Altitude Monitor ................................................................ 1-8 ADS-B Monitor ................................................................. 1-9 1.7 Warning Messages .......................................................... 1-9 1.8 Fault Annunciation ........................................................... 1-9 1.9 Configuration Mode ....................................................... 1-10 1.10 Low Temperature Operation ......................................... 1-10
2. Appendix ................................................................................. 2-1
2.1 Acronyms and Abbreviations ........................................... 2-1
KT 74 Pilot's Guide
Table of Contents
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List of Illustrations
Figure Page Figure 1-1: Front Panel Controls and Functions ............................. 1-2 Figure 1-2: Display .......................................................................... 1-2 Figure 1-3: Mode Knob ................................................................... 1-4 Figure 1-4: Push Buttons ................................................................ 1-5 Figure 1-5: Functions ...................................................................... 1-6
List of Tables
Table 1-1: FUNC Sequence with Squat Switch Input Enabled ....... 1-7 Table 1-2: FUNC Sequence without Squat Switch Input Enabled .. 1-7
KT 74 Pilot's Guide
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Operation Rev 0 Dec 2013
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1. OPERATION
1.1 INTRODUCTION Congratulations on choosing the KT 74 ADS-B Out Enabled Mode S Transponder. At BendixKing we are committed to providing you with the most reliable and advanced technology that will meet your transponder needs. The KT 74 meets the Global Mandates for Automatic Dependent Surveillance – Broadcast (ADS-B) out* and more.
*When coupled with approved GPS source, STC and install kit required.
Additional KT 74 Benefits:
•
Push button operation •
New sleek design •
Most affordable Mode S Transponder with ADS-B Out •
Low power consumption •
Stopwatch and timer •
Altitude monitor •
Built-in altitude repeater instead of a second altitude encoder • TIS-A Traffic output
The feature-rich KT 74 brings the value, simplicity, reliability and affordability into the cockpit that BendixKing has been trusted for since 1959.
The KT 74 is certified to ETSO C112d Class 1 Mode S level 2els, ETSO C166b Class B1S, FAA TSO C112D and TSO C166B.
KT 74 Pilot's Guide
Operation
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© Honeywell International Inc. Do not copy without express permission of Honeywell
1.2 FRONT PANEL CONTROLS AND FUNCTIONS
Figure 1-1: Front Panel Controls and Functions
The KT 74 has the following front panel controls and functions:
•
Display: See section 1.3. •
Mode Knob: See section 1.4. •
Push Buttons: See section 1.5. • Functions: See section 1.6.
1.3 DISPLAY
Figure 1-2: Display
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The display shows the following indications:
•
Active Mode: the Active Mode indicator shows the mode that is currently set on the Mode Knob. See section 1.4. • Pressure Altitude: The reported pressure altitude is
displayed as a Flight Level (FL), which is the pressure altitude in hundreds of feet. When non-standard atmospheric conditions apply, this may not match the altimeter indicated altitude, but will be correctly displayed by the Air Traffic Control (ATC) radar.
• Squawk Code: The current squawk code selected by the Numeric Buttons. See Squawk Code Entry in section 1.5
• Flight ID: The aircraft call sign entered on your flight plan. See Flight ID Entry in section 1.6
• IDENT Indicator: The IDENT Indicator shows when IDENT mode is active. See section 1.5.
• Reply Indicator : The Reply Indicator is active when the transponder replies to interrogations.
• Deviation Pointer: When altitude monitoring is in use, a small deviation pointer appears adjacent to the altitude display on the transponder. See Altitude Monitor in section 1.6.
• Warning message: See section 1.7
•
Fault Annunciation: See section 1.8. Light Sensor
If connected to a lighting bus, the KT 74 will adjust the brightness of the front panel lighting based upon the lighting bus input. If no lighting bus input is detected, the KT 74 will automatically control the front panel lighting based on the ambient light sensor. The dim point for the Liquid Crystal Display (LCD) backlight illumination can be adjusted by using the configuration mode as described in section 1.9 of this guide.
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Operation
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© Honeywell International Inc. Do not copy without express permission of Honeywell
1.4 MODE KNOB
Figure 1-3: Mode Knob
The mode knob to the right of the display controls the power to the transponder and the operating mode. The mode knob has the selections that follow:
OFF
Power is removed from the transponder. SBY
The transponder is on, but will not reply to any interrogations. ON The transponder will respond to all interrogations, but
altitude reporting is suppressed.
ALT
The transponder will respond to all interrogations. When airborne, the transponder should always be set to ALT unless otherwise directed by Air Traffic Control. Aircraft installations that include a gear squat switch or other method of air/ground determination will automatically select surface reporting mode on
landing or when taxiing. The mode indicator will read GND.
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1.5 PUSH BUTTONS
Figure 1-4: Push Buttons
IDENT
Press the IDENT button when ATC instructs you to “Ident” or “Squawk Ident”. This activates the SPI pulse in the transponder replies for 18 seconds. IDENT will appear in the display.
VFR
Pressing the VFR button sets the transponder to the pre-programmed VFR code. Pressing the button again restores the previous squawk code.
Pressing the VFR button while in Flight ID editing mode changes the Flight ID to the pre-programmed ID set up during configuration of the transponder.
FUNC
Pressing the FUNC button provides access to the flight timer, stopwatch, Flight ID entry, ADS-B monitor (depending on installation) and altitude monitor function. See section 1.6 below.
ENT The ENT button confirms selection or presented options. 0-7 The numeric buttons are used to change the squawk code and as part of the data entry selections.
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Squawk Code Entry
Press any of the numeric buttons (0 through 7) to change the squawk code. A new squawk code is set when the fourth digit is entered. If the code entry is not completed within 7 seconds, the changes are ignored and the previous code restored. Some standard squawk codes are listed below:
• 1200 VFR code in the USA
• 7000 VFR code commonly used in Europe • 7500 Hijack code
• 7600 Loss of communications •
7700
Emergency code
1.6 FUNCTIONS
Figure 1-5: Functions
The different KT 74 functions are accessed using the FUNC button. The functions displayed vary depending on whether the aircraft is airborne or is on the ground (squat switch or other method of air/ground determination installed) and has the GPS input enabled or not as shown in the following tables.
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Table 1-1: FUNC Sequence with Squat Switch Input Enabled Airborne/ Ground GPS INPUT SEQUENCE
Airborne
Yes
PWR ON (Squawk) -> Flight Time -> Timer -> ADS POS -> Edit Flight ID -> Alt Monitor -> Squawk
Airborne No PWR ON (Squawk) -> Flight Time -> Timer -> Edit Flight ID -> Alt Monitor -> Squawk On
Ground Yes PWR ON (Squawk) -> Flight Time -> Timer -> ADS POS -> Edit Flight ID -> Squawk On
Ground
No
PWR ON (Squawk) -> Flight Time -> Timer -> Edit Flight ID -> Squawk
Table 1-2: FUNC Sequence without Squat Switch Input Enabled GPS INPUT SEQUENCE
Yes PWR ON (Squawk) -> Flight Time -> Timer -> ADS POS -> Edit Flight ID -> Alt Monitor -> Squawk No PWR ON (Squawk) -> Flight Time -> Timer -> Edit Flight ID -> Alt Monitor -> Squawk
Each function is described in more detail below:
Flight Timer
Press the FUNC button once to display the Flight Timer. The Flight Timer records the time for which the transponder has been powered on and operating in flight mode – either ON or ALT .
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Stopwatch
Press the FUNC button twice to display the stopwatch. The stopwatch can be used as a convenient timer. Pressing ENT will reset and start the timer. Pressing ENT again will stop the timer.
Flight ID Entry
Press the FUNC button three times to display the Flight ID entry screen. The edit the Flight ID using the numeric buttons. The lower portion of the display shows the alpha numeric characters selected through multiple presses of the numeric buttons. When the correct character is shown in the flight ID section of the screen, press the ENT button to accept and advance to the next digit. The flight ID is terminated with a “space” character located on the 7 button. When ENT is pressed on the end space, the new Flight ID will replace the previous value. If a button is not pressed for 7 seconds, the changes are ignored and the previous code restored.
The Flight ID should correspond to the aircraft call sign entered on your flight plan. If no flight plan is active, the aircraft registration should be used as your Flight ID. Use only letters and digits. If the Flight ID is less than 8 characters long, enter the “space” character (7 button) to end it.
Altitude Monitor
Press the FUNC button four times to display the Altitude Monitor enable screen. The Altitude Monitor activates an audio annunciator or annunciator light (depending on installation) when the aircraft pressure altitude differs from the selected altitude by more than 200 feet. Pressing ENT toggles the altitude monitor at the current altitude.
When altitude monitoring is in use, a small deviation pointer appears adjacent to the altitude display on the transponder.
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ADS-B Monitor
Press the FUNC button five times to display the Altitude Monitor screen The ADS-B Monitor is only available on installations that include an ADS-B position source. The ADS-B Monitor provides a display of the position information that is being transmitted in ADS-B position reports. This can provide confirmation that the correct information is being transmitted, particularly where the Global Positioning System (GPS) source is remote from the transponder. In the event that valid position information is NOT available from the GPS, the latitude and longitude display will be replaced by dashes. If no valid latitude and longitude is shown, then ADS-B position information is NOT being transmitted.
Loss of ADS-B position information will also result in a WARNING message being displayed.
1.7 WARNING MESSAGES
If the transponder detects a problem, the screen will indicate WARNING and a brief statement of the problem. Depending on the nature of the problem, your transponder may not be replying to interrogations. Note the message on the screen and pass that information to your avionics maintenance organization. The WARNING message should clear when the event has cleared. Press ENT to clear the message at any time; if the fault is still present the message may reappear.
1.8 FAULT ANNUNCIATION
If the transponder detects an internal failure, the screen will indicate FAULT and a brief statement of the problem. No replies will be made to interrogations when a fault is detected.
Some FAULT indications can be recovered by switching the transponder off and back on again, although in all cases a FAULT code implies that there is a fault with the transponder or the installation. Note the FAULT message at the bottom of the screen and pass that information to your avionics maintenance organization.
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1.9 CONFIGURATION MODE
The system is configured when it is first installed by your avionics installer. Configuration items include the Mode S aircraft address, the interface to the other aircraft systems, the aircraft category, and the pre-programmed values for VFR squawk code. To view or change these settings you must use Configuration Mode.
Do not use Configuration Mode in flight. Check with your avionics installer before changing the configuration.
To enter configuration mode, hold down the FUNC button while switching on the transponder. Configuration items can be changed using the numeric buttons (6 for down, 7 for up) and the ENT button to accept the selection. Pressing the 2 button will move back to the last menu item. Pressing FUNC advances to the next configuration item.
When configuration is complete; switch the transponder off. When it is switched back on the transponder will use the new configuration.
1.10 LOW TEMPERATURE OPERATION
The KT 74 is certified to operate down to -25°C; however under cold operating conditions, the display update rate may be slowed but functional. The KT 74 incorporates an integral heating element in the front panel to automatically raise the temperature around the display. During cold operating conditions, a warm up period of 5 minutes minimum is suggested.
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2. APPENDIX
2.1
ACRONYMS AND ABBREVIATIONS
Acronyms and abbreviations used in this manual are defined as follows: TERMS DEFINITION
ADS-B Automatic Dependent Surveillance ‐Broadcast ALT Altitude
ATC Air Traffic Control ENT Enter
FAA Federal Aviation Administration FL Flight Level FUNC Function
GPS Global Positioning System ID
Identification IDENT Identify
LCD Liquid Crystal Display SBY Standby
VFR Visual Flight Rules
Copyrighted information in this manual is subject to change without notice. Bendix/King reserves the right to improve or change the products or contents of this manual, without notification of any person or agency. The contents of this pilot's guide may be downloaded, stored and reprinted for personal use provided that this copyright information is included. Commercial use is strictly prohibited. For further information contact **************************.。